Aircraft turbine engine control systems development: Historical Perspective

被引:0
|
作者
Lutambo, Jackson [1 ]
Wang, Jiqiang [1 ,2 ]
Yue, Hong [3 ]
Dimirovsky, Georgi [4 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Nanjing 210016, Jiangsu, Peoples R China
[2] AVIC Shenyang Engine Design & Res Inst, Shenyang 110015, Peoples R China
[3] Univ Strathclyde, Glasgow, Lanark, Scotland
[4] Dogus Univ Istanbul, Istanbul, Turkey
关键词
Control system; Gas Turbine Engine; Hydromechanical System; FullAuthority Digital Electronic Control (FADEC); Digital Electronic Engine Control (DEEC);
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper describes the development of aircraft turbine engine control systems from the historical point of view to the present. With the increasing emphasis on aircraft safety, enhanced performance, and affordability, as well as the need to reduce the environmental effect caused by aircraft, there are many new challenges being faced by the designers of aircraft propulsion systems. The paper provides an overview of the various technological development activities in aircraft engine control and diagnostics, both current and some accomplished in the recent past. The motivations for each of the research efforts, the research approach, technical challenges, and the key progress to date are summarized.
引用
收藏
页码:5736 / 5741
页数:6
相关论文
共 50 条
  • [31] ROTARY COMBUSTION ENGINE IS AS NEAT AND TRIM AS AIRCRAFT TURBINE
    JONES, C
    SAE JOURNAL, 1968, 76 (05): : 67 - &
  • [32] Leak detection in the lubrication system of an aircraft turbine engine
    Rakoto, L.
    Kinnaert, M.
    Strengnart, M.
    Raimarckers, N.
    ADVANCES IN SAFETY, RELIABILITY AND RISK MANAGEMENT, 2012, : 566 - 571
  • [33] Nonlinear modelling and validation of an aircraft gas turbine engine
    Chiras, N
    Evans, C
    Rees, D
    NONLINEAR CONTROL SYSTEMS 2001, VOLS 1-3, 2002, : 871 - 876
  • [34] AIRCRAFT ENGINE TURBINE-BLADES RECONDITIONED BY HARDFACING
    PEREMILOVSKII, IA
    GEICHENKO, VS
    FRUMIN, II
    AUTOMATIC WELDING USSR, 1976, 29 (05): : 40 - 42
  • [35] Transition of a technology base for advanced aircraft gas turbine control systems
    McGlone, ME
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1998, 120 (03): : 437 - 441
  • [36] Characterization of aircraft gas turbine engine particle emissions
    Timko, Michael T.
    Yu, Zhenhong
    Wong, Hsi-Wu
    Miake-Lye, Richard C.
    Onasch, Timothy
    Jayne, John T.
    Canagaratna, Manjula R.
    Herndon, Scott C.
    Wood, Ezra C.
    ABSTRACTS OF PAPERS OF THE AMERICAN CHEMICAL SOCIETY, 2009, 237
  • [37] ADVANCED AIRCRAFT GAS-TURBINE ENGINE CONTROLS
    WRIGHT, WE
    HALL, JC
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1990, 112 (04): : 561 - 564
  • [38] Gas turbine unit based on aircraft converted engine
    Reznik, VE
    Gorelov, GM
    Danilchenko, VP
    IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1995, (04): : 66 - 70
  • [39] SMALL TURBINE ENGINE INTEGRATION IN AIRCRAFT INSTALLATIONS.
    Botman, M.
    Blinco, R.K.
    AGARD Conference Proceedings, 1978, (248): : 1 - 23
  • [40] Transient performance simulation of aircraft engine integrated with fuel and control systems
    Wang, C.
    Li, Y. G.
    Yang, B. Y.
    APPLIED THERMAL ENGINEERING, 2017, 114 : 1029 - 1037